MARS EXPRESS SPICAM GEOMETRY FILES Description =========================================================================== Revisions -------------------------------------------------------- 2008 03 10 V013 correction following new geometry file version (V14) 2007 07 08 V012 correction following new geometry file version (V13) 2005 11 18 V011 correction following new geometry file version (V10) 2004 10 12 V010 initial dimarellis Purpose This document describes the contents of the geometry files which are delivered in the Spicam data product. Introduction =========================================================================== All informations needed to read the geometry file are given. This document is organized as: Introduction Overview Header contents Definitions Computation background Overview: =========================================================================== The geometry file is an ASCII file. For each UV or IR data file, a geometry file is computed. The geometrical parameters are computed at the time of the UV or IR data (which is not the time of the measurement itself, see SPICAM_UVCALIB_DESC.TXT) This file is computed with SPICE/Naif tools and kernels. The ASCII file is made of 2 parts: a header part a list of parameters, one row for each time The header is easily readable and gives all informations on the parameters. Header contents: =========================================================================== The following informations are listed in the header: Software version and date used for computation Filename List of SPICE kernels SUN information at the first time of the file Target (STAR, SUN, NADIR/LIMB, ...) Positions on the CCD Parameters list and meaning Definitions: =========================================================================== Though the file is self documented, the following definitions are useful. Altitude Computed with MARS ellipsoid (Spice kernel) Longitude positive eastward LOS Line of Sight, this line is related to the center of CCD row 144 MNP Mars Nearest Point of the LOS 1stB, 2ndB, 3rdB, 4thB, and 5thB are center of UV Bands (binning included) The IR LOS corresponds to the 3rdB LOS (IR FOV is 1 deg) EMEJ2000 Earth Mean Equator, dynamical equinox of J2000. MarsJ2000 MARSIAU frame (Mars Mean Equator and IAU vector of J2000). MEX Mars Express Computation background: =========================================================================== The computation of geometrical parameters is TARGET dependant. For point source (STAR) ----------------------- The LOS and 1stdB, 2nddB,3rdB,4thdB and 5thdB parameters are computed. The Line of sight is fully defined by the spacecraft position and the direction of the star. So, attitude file is not needed to compute most of parameters. For 1stB, 2ndB, 3rdB, 4thB, and 5thB, we need to know the S/C X axis, and now we need the attitude file. For extended sources (NADIR, LIMB, SUN) -------------------------------------- The 1stdB, 2nddB,3rdB,4thdB and 5thdB parameters are computed. To compute geometrical parameters, we need to read the attitude file which gives the directions of the S/C axes. For more details about the geometry computation, please read the SPICAM_POINTING_xxx.TXT file.